Linearization in satellite attitude control with modified Rodriguez parameters

Doruk R. O.

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, cilt.81, sa.3, ss.199-203, 2009 (SCI-Expanded) identifier identifier

  • Yayın Türü: Makale / Tam Makale
  • Cilt numarası: 81 Sayı: 3
  • Basım Tarihi: 2009
  • Doi Numarası: 10.1108/00022660910954691
  • Dergi Adı: AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY
  • Derginin Tarandığı İndeksler: Science Citation Index Expanded (SCI-EXPANDED), Scopus
  • Sayfa Sayıları: ss.199-203
  • Anahtar Kelimeler: Kinematics, Control technology, Space technology, Artificial satellites
  • Orta Doğu Teknik Üniversitesi Adresli: Hayır

Özet

Purpose - The purpose of this paper is to analyze the results of the Jacobian matrix linearization of the satellite attitude dynamics with modified Rodriguez parameters (MRP) as attitude representation.